Stand for testing ram-BRAKE launch complex at real loading conditions

摘要

The invention relates to test equipment, in particular to a stand for testing power gidropnevmooborudovaniya at real load conditions, for use on the starting missile systems, and can be used in tests of hydraulic jacks, the brakes (SDT) of different sizes, and gidrobuferov, pnevmogidroamortizatorov, and damper jacks average power geared plunger 600 mm.; The technical problem to be solved by the utility model is to create a test bench for hydraulic jacks, brakes launch complex of a wide range, providing full-scale load conditions with minimal rework known stand.; The main element of the stand, providing SDT loading test, the pendulum is designed as a lever, rotatably mounted in bearing units mounted on horizontal beams portal mounted under the stand. On the lever attached basket with removable weights. To the upper portion of the lever is fixed an additional lever, on the distal end of which is housed the second basket with exchangeable weights, and the longitudinal axis of the levers coincide. The lower and upper baskets mounted loads, the number of which is determined by calculation from the condition may better align the inertial pendulum and static parameters of the charging device and the protected-brake hydraulic jack object. The lever is connected with a cable winch, designed to deflect the pendulum, changing its tilt angle and hold it at a predetermined angle of inclination. The free end of the rope is attached to the lock bottom basket.; When tested situ loading conditions of the test are provided by the equation SDT static moment and the moment of inertia of the pendulum loading device stand relevant characteristics of the protected object SDT-kind.; The proposed utility model allows accurate evaluation of performance jacks, brakes, members of the modernized existing and future launch complexes.